3D inverse method for turbomachine blading with splitter blades

X. Qiu, Thong Q Dang

Research output: Chapter in Book/Report/Conference proceedingConference contribution

6 Scopus citations

Abstract

The use of a full 3D and viscous inverse method for turbomachine blading with splitter blades is demonstrated by carrying out a design modification of a transonic axial stator blade row with splitter blades. In this design modification study, the goal is to improve the aerodynamics of the full blade and the splitter blade, including weakening of shock wave and control of flow incidence. The improved blade design is "validated" using a well-known 3D Navier-Stokes analysis solver.

Original languageEnglish (US)
Title of host publicationAircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery
PublisherAmerican Society of Mechanical Engineers (ASME)
Volume1
ISBN (Print)9780791878545, 9780791878545
DOIs
StatePublished - 2000
EventASME Turbo Expo 2000: Power for Land, Sea, and Air, GT 2000 - Munich, Germany
Duration: May 8 2000May 11 2000

Other

OtherASME Turbo Expo 2000: Power for Land, Sea, and Air, GT 2000
CountryGermany
CityMunich
Period5/8/005/11/00

ASJC Scopus subject areas

  • Engineering(all)

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  • Cite this

    Qiu, X., & Dang, T. Q. (2000). 3D inverse method for turbomachine blading with splitter blades. In Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery (Vol. 1). American Society of Mechanical Engineers (ASME). https://doi.org/10.1115/2000-GT-0526